Marine vessel fuel overflow tank system

• US 20040261899A1
• Filed: 06/11/2003
• Published: 12/30/2004
• Est. Priority Date: 06/11/2003
• Status: Active Grant

• Current Assignee: Stephen P. Vaitses
• Original Assignee: Stephen P. Vaitses
• Inventors: Vaitses, Stephen P.
• Granted Patent: US 6,929,039 B2
• Time in Patent Office: Days
• US Class Current: 141/311.00A
• CPC Class Codes: B63B 11/04 Constructional features of bunkers, e.g. structural fuel tanks, or ballast tanks, e.g. with elastic walls tanks for fuel or the like not forming subdivisions of the hull B63B17/0027; cleaning of tanks B63B57/00

Abstract

A marine vessel overflow tank system for use in the hull of a marine vessel that has a fuel system including a fuel vent line connecting a fuel tank to a vent that communicates with the atmosphere. The system comprises a first vent line fitting adapted for direct parallel communication with the fuel vent line. The internal cross sectional area of the first vent line fitting is approximately the same size as the internal cross sectional area of the fuel vent line. The system also comprises a second vent line fitting adapted for direct parallel communication with the fuel vent line. The internal cross sectional area of the second vent line fitting is approximately the same size as the internal cross sectional area of the fuel vent line. The system further comprises a fuel expansion tank. The fuel expansion tank comprises a plurality of walls defining an enclosed chamber and a first restrictive orifice located in one the walls. The first orifice is in direct communication with the first vent line fitting and has an internal cross sectional area less than the internal cross sectional area of the fuel vent line. The fuel expansion tank also comprises a second restrictive orifice located in one the walls defining the enclosed chamber. The second restrictive orifice is in direct communication with the second vent line fitting and has an internal cross sectional area less than the internal cross sectional area of the fuel vent line. The fuel expansion tank further comprises means for attaching the chamber to the hull with the first restrictive orifice being positioned above the second restrictive orifice and proximate to a top edge of the chamber, and the second restrictive orifice being positioned above the fuel tank and proximate to a bottom edge of the chamber.

Claims

1. A marine vessel fuel overflow tank system for use in the hull of a marine vessel that has a fuel system including a fuel vent line connecting a fuel tank to a vent that communicates with the atmosphere, said system comprising:

a first vent line fitting adapted for direct parallel communication with the fuel vent line, wherein the internal cross sectional area of said first vent line fitting is approximately the same size as the internal cross sectional area of said fuel vent line;

a second vent line fitting adapted for direct parallel communication with the fuel vent line, wherein the internal cross sectional area of said second vent line fitting is approximately the same size as the internal cross sectional area of said fuel vent line; and

a fuel expansion tank comprising;

a plurality of walls defining an enclosed chamber;

a first restrictive orifice located in one of said walls in direct communication with said first vent line fitting, wherein said first restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line;

a second restrictive orifice located in one of said walls in direct communication with said second vent line fitting, wherein said second restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line; and

means for attaching said chamber to the hull with said first restrictive orifice being positioned above said second restrictive orifice and proximate to a top edge of said chamber, and said second restrictive orifice being positioned above said fuel tank and proximate to a bottom edge of said chamber.

2. The system of claim 1 further comprising a first and second length of flexible tubing, wherein said first restrictive orifice is in direct communication with said first vent line fitting via said first length of flexible tubing and said second restrictive orifice is in direct communication with said second vent line fitting via said second length of flexible tubing.

3. The system of claim 1 wherein said chamber includes a plurality of plugged restrictive orifices, wherein said first restrictive orifice and said second restrictive orifice are selected from said plurality of plugged restrictive orifices and the plugs corresponding to said first restrictive orifice and said second restrictive orifice are removed.

4. The system of claim 1 wherein said first vent line fitting and said second vent line fitting do not obstruct said fuel vent line when in direct parallel communication with said fuel vent line.

5. The system of claim 1 wherein said first vent line fitting and said second vent line fitting are T-shaped.

6. The system of claim 1 wherein the internal cross sectional area of said first restrictive orifice restricts the maximum flow rate through said first orifice for limiting an amount of fuel from entering said fuel expansion tank via said first restrictive orifice during refueling of the fuel tank;

and

the internal cross sectional area of said second restrictive orifice restricts the maximum flow rate through said second orifice for limiting an amount of fuel from entering said fuel expansion tank via said second restrictive orifice during refueling of the fuel tank.

7. The system of claim 1 wherein the internal cross sectional area of said first restrictive orifice is the same as the internal cross sectional area of said second restrictive orifice.

8. The system of claim 1 wherein the internal cross sectional area of said first restrictive orifice is less than the internal cross sectional area of said second restrictive orifice.

9. The system of claim 1 wherein the internal cross sectional area of said second restrictive orifice is between about one-eighth of the internal cross sectional area of the fuel vent line and about one-sixteenth of the internal cross sectional area of the fuel vent line.

10. The system of claim 1 wherein said first restrictive orifice has a diameter between about three thirty-seconds of an inch and about one-quarter of an inch.

11. The system of claim 1 wherein said second restrictive orifice has a diameter between about three thirty-seconds of an inch and about one-quarter of an inch.

12. The system of claim 1 wherein said plurality of walls are aluminum.

13. The system of claim 1 wherein said enclosed chamber is rectangular in shape.

14. The system of claim 1 wherein said enclosed chamber is cylindrical in shape.

15. The system of claim 1 wherein the means for attaching said chamber includes metal brackets.

16. The system of claim 1 wherein the enclosed chamber is adapted to contain gasoline.

17. The system of claim 1 wherein the enclosed chamber is adapted to contain diesel.

18. The system of claim 1 further comprising a control valve attached to said second restrictive orifice for varying the effective internal cross sectional area of said second restrictive orifice.

19. In combination, a fuel system and a fuel expansion tank for use in the hull of a marine vessel, the fuel system comprising:

a fuel tank;

a filler tube open to said fuel tank for delivering fuel to the fuel tank; and

a fuel vent line in fluid communication with the fuel tank and the atmosphere, the fuel vent line including a first vent line fitting and a second vent line fitting both adapted for direct parallel communication with the fuel expansion tank; and

the fuel expansion tank comprising;

a plurality of walls defining an enclosed chamber;

a first restrictive orifice located in one of said walls in direct parallel communication with said first vent line fitting, wherein said first restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line;

a second restrictive orifice located in one of said walls in direct parallel communication with said second vent line fitting, wherein said second restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line; and

means for attaching said chamber to the hull with said first restrictive orifice being positioned above said second restrictive orifice and proximate to a top edge of said chamber, and said second restrictive orifice being positioned above said fuel tank and proximate to a bottom edge of said chamber.

20. The combination of claim 19 wherein:

the internal cross sectional area of said first restrictive orifice restricts the maximum flow rate through said first orifice for limiting an amount of fuel from entering said fuel expansion tank via said first restrictive orifice during refueling of the fuel tank; and

the internal cross sectional area of said second restrictive orifice restricts the maximum flow rate through said second orifice for limiting an amount of fuel from entering said fuel expansion tank via said second restrictive orifice during refueling of the fuel tank.

21. The combination of claim 19 wherein said second restrictive orifice is positioned to allow the contents of said expansion tank to drain into the fuel tank via the fuel vent line.

22. A method of utilizing a fuel expansion tank in the hull of a marine vessel that has a fuel system including a fuel vent line connecting a fuel tank to a vent that communicates with the atmosphere, wherein the fuel vent line includes a first vent line fitting and a second vent line fitting both adapted for direct parallel communication with the fuel expansion tank, the method comprising:

attaching the fuel expansion tank to the marine vessel, wherein the fuel expansion tank includes;

a plurality of walls defining an enclosed chamber;

a first restrictive orifice located in one of said walls in direct communication with said first vent line fitting, wherein said first restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line;

a second restrictive orifice located in one of said walls in direct communication with said second vent line fitting, wherein said second restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line; and

means for attaching said chamber to the hull with said first restrictive orifice being positioned above said second restrictive orifice and proximate to a top edge of said chamber, and said second restrictive orifice being positioned above said fuel tank and proximate to a bottom edge of said chamber;

attaching said first vent line fitting to said first restrictive orifice;

attaching said second vent line fitting to said second restrictive orifice;

wherein, if the fuel vent line is filled to a level at or above said first restrictive orifice then receiving fuel into said fuel expansion tank via said first restrictive orifice;

wherein, if the fuel vent line is filled to a level at or above said second restrictive orifice then receiving the fuel into said fuel expansion tank via said second restrictive orifice;

wherein, if the fuel vent line is filled to a level at or above said second restrictive orifice and below said first restrictive orifice then venting vapor and air out of said first restrictive orifice;

wherein, if the fuel vent line is filled to a level below said second restrictive orifice then draining the fuel from said fuel expansion tank into the fuel vent line via said second restrictive orifice; and

wherein, if the fuel vent line is filled to capacity and more fuel is flowing into said fuel vent line at a rate higher than the maximum flow rate of said first restrictive orifice and said second restrictive orifice then venting the fuel from said fuel vent line into the vent.

23. A fuel expansion tank for use in the hull of a marine vessel that has a fuel system including a fuel vent line connecting a fuel tank to a vent that communicates to the atmosphere, said fuel expansion tank comprising:

a plurality of walls defining an enclosed chamber;

a first restrictive orifice located in one of said walls and adapted for direct parallel communication with the fuel vent line, wherein said first restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line;

a second restrictive orifice located in one of said walls and adapted for direct parallel communication with the fuel vent line, wherein said second restrictive orifice has an internal cross sectional area less than the internal cross sectional area of the fuel vent line; and

means for attaching said chamber to the hull with said first restrictive orifice being positioned above said second restrictive orifice and proximate to a top edge of said chamber, and said second restrictive orifice being positioned above said fuel tank and proximate to a bottom edge of said chamber.